Nonlinear analysis of laminated shells with alternating stiff/soft lay-up

被引:11
|
作者
Liang, Y. [1 ]
Izzuddin, B. A. [1 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Civil & Environm Engn, London SW7 2AZ, England
关键词
Multi-layer; Alternating stiff/soft lay-up; Zigzag effect; Transverse shear strain; Large displacement; SANDWICH PLATES; ZIGZAG FUNCTIONS; FINITE-ELEMENT; COMPOSITE; DEFORMATION; FORMULATION; MITC9;
D O I
10.1016/j.compstruct.2015.08.043
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper proposes a multi-layer formulation for the nonlinear analysis of laminated shells with an alternating stiff/soft lay-up. The zigzag variation of planar displacements is taken into account by adding to the Reissner-Mindlin formulation a specific set of zigzag function which is effective for the considered lay-up. Furthermore, a piecewise linear through-thickness distribution of the material transverse shear strain is assumed, which agrees well with the real distribution. The proposed lamination model with a low-order nonlinear strain-displacement relationship is incorporated within a co-rotational framework for geometric nonlinear analysis, thus upgrading the low-order local element formulation to large displacement analysis with relative ease. In addition, a local shell system is employed for direct definition of the additional zigzag displacement fields and associated parameters, which are thus excluded from the large displacement co-rotational transformations. The application of the proposed laminated shell modelling approach is illustrated in this paper for a 9-noded co-rotational shell element, which utilises the Mixed Interpolation of Tensorial Components (MITC) method in the local system for overcoming locking effects. Several linear and nonlinear numerical examples of multi-layer shell structures with alternating stiff/soft lay-ups are used to illustrate the effectiveness and efficiency of the proposed modelling approach. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1220 / 1236
页数:17
相关论文
共 50 条
  • [1] Analysis of tapered laminated composites with non-symmetric lay-up
    Varughese, B
    Mukherjee, A
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1997, 16 (07) : 631 - 660
  • [2] Hybrid laminated composites molded by spray lay-up process
    Xiao, Bing
    Yang, Yuqiu
    Wu, Xiaofeng
    Liao, Mengyuan
    Nishida, Ryuiti
    Hamada, Hiroyuki
    [J]. FIBERS AND POLYMERS, 2015, 16 (08) : 1759 - 1765
  • [3] Lay-up independent fracture criterion for notched laminated composites
    Lee, Bokwon
    Sankar, Bhavani V.
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (14) : 2491 - 2499
  • [4] Hybrid laminated composites molded by spray lay-up process
    Bing Xiao
    Yuqiu Yang
    Xiaofeng Wu
    Mengyuan Liao
    Ryuiti Nishida
    Hiroyuki Hamada
    [J]. Fibers and Polymers, 2015, 16 : 1759 - 1765
  • [5] Analysis and Lay-up Optimization for Vibration of Laminated Plates with Complex Shape and Edge Conditions
    Narita, Yoshihiro
    Honda, Shinya
    Owatari, Kosuke
    [J]. INTERNATIONAL CONFERENCE ON MECHANICS AND MATERIALS ENGINEERING (ICMME 2014), 2014, : 436 - 442
  • [6] Designability analysis of the dynamics of thin-walled carbon fiber laminated shells based on varying the lay-up angle and number of plies
    Zhang, Daqian
    Yuan, Haochen
    [J]. AIP ADVANCES, 2021, 11 (12)
  • [7] On feasible regions of lamination parameters for lay-up optimization of laminated composites
    Bloomfield, M. W.
    Diaconu, C. G.
    Weaver, P. M.
    [J]. PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2009, 465 (2104): : 1123 - 1143
  • [8] The effect of ply lay-up upon the thermoelastic response of laminated composites
    Cunningham, PR
    Dulieu-Barton, JM
    Dutton, AG
    Shenoi, RA
    [J]. EXPERIMENTAL TECHNIQUES AND DESIGN IN COMPOSITE MATERIALS 5, 2002, 221-2 : 325 - 335
  • [9] Effect of lamination anisotropy and lay-up in glued-laminated timbers
    Aicher, S
    Dill-Langer, G
    [J]. JOURNAL OF STRUCTURAL ENGINEERING-ASCE, 2005, 131 (07): : 1095 - 1103
  • [10] STIFFENED COMPOSITE AXISYMMETRICAL SHELLS OPTIMUM LAY-UP FOR BUCKLING BY RANKING
    TRIPATHY, B
    RAO, KP
    [J]. COMPUTERS & STRUCTURES, 1993, 46 (02) : 299 - 309